Federal Aviation Administration January 14, 2016 – Federal Register Recent Federal Regulation Documents

Eighth Meeting: RTCA Special Committee (231) Terrain Awareness Warning Systems (TAWS)
Document Number: 2016-00625
Type: Notice
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of the Eighth RTCA Special Committee 231 meeting.
Twenty-Fifth Meeting: RTCA Special Committee (217) Aeronautical Databases (Joint With EUROCAE WG-44)
Document Number: 2016-00624
Type: Notice
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of the Twenty-Fifth RTCA Special Committee 217 meeting.
Sixth Meeting: RTCA Special Committee (232) Airborne Selective Calling Equipment
Document Number: 2016-00623
Type: Notice
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of the Sixth RTCA Special Committee 232 meeting.
Commercial Space Transportation Advisory Committee-Public Teleconference
Document Number: 2016-00620
Type: Notice
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of a teleconference of the Commercial Space Transportation Advisory Committee (COMSTAC). The Teleconference will take place on Wednesday, January 27, 2016 starting at 3:00 p.m. Eastern Standard Time and will last approximately one hour. The agenda and call-in number will be posted at least one week in advance at http://www.faa.gov/go/ ast. The purpose of this teleconference is to review the International Space Policy Working Group findings and recommendations regarding a potential modification of current U.S. policy on the launching of U.S. technology on Indian launch vehicles. Interested members of the public may submit relevant written statements for the COMSTAC members to consider under the advisory process. Statements may concern the issues and agenda items mentioned above and/or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Michael Beavin, COMSTAC Executive Director, (the Contact Person listed below) in writing (mail or email) by January 22, 2016, so that the information can be made available to COMSTAC members for their review and consideration before the January 27 teleconference. Written statements should be supplied in the following formats: One hard copy with original signature and/or one electronic copy via email. An agenda will be posted on the FAA Web site at www.faa.gov/go/ast. Individuals who plan to participate and need special assistance should inform the Contact Persons listed below in advance of the meeting.
Amendment of United States Area Navigation (RNAV) Route Q-35, Western United States
Document Number: 2015-33095
Type: Rule
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
This action makes an editorial change to the legal description of United States Area Navigation Route Q-35 to reverse the order of points listed in the route description in FAA Order 7400.9. This action is simply to comply with the standard format for describing routes. The existing alignment of the airway is not affected by this action.
Airworthiness Directives; Airbus Airplanes
Document Number: 2015-32519
Type: Rule
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2004-14-09 for certain Airbus Model A320-211, -212, and -231 airplanes. AD 2004-14-09 required repetitive inspections for fatigue cracking of the lower surface panel on the wing center box, and repair if necessary; and modification of the lower surface panel on the wing center box, which constitutes terminating action for the repetitive inspections. This new AD retains the requirements of AD 2004-14-09, reduces the compliance times for the repetitive inspections, and requires an additional repair for certain airplanes. This AD was prompted by a determination that, based on the average flight duration, the average weight of fuel at landing is higher than that defined for the analysis of the fatigue-related tasks; and that shot peening might have been improperly done on the chromic acid anodizing (CAA) protection, which would adversely affect fatigue crack protection. We are issuing this AD to detect and correct fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane.
Stage 5 Airplane Noise Standards
Document Number: 2015-32500
Type: Proposed Rule
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
This action would establish a new noise standard for certain subsonic jet airplanes and subsonic transport category large airplanes. This noise standard, known as Stage 5, would apply to any person submitting an application for a new airplane type design with a maximum certificated takeoff weight of 121,254 pounds (55,000 kg) or more on or after December 31, 2017; or with maximum certificated takeoff weight of less than 121,254 pounds (55,000 kg) on or after December 31, 2020. This change would reduce the noise produced by new airplanes and harmonize the noise certification standards for those airplanes certificated in the United States with the new International Civil Aviation Organization noise standard in Annex 16, Chapter 14, effective July 14, 2014.
Airworthiness Directives; Fokker Services B.V. Airplanes
Document Number: 2015-32259
Type: Rule
Date: 2016-01-14
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 1000, 2000, 3000, and 4000 airplanes. This AD was prompted by a design review, which revealed that no controlled bonding provisions are present on a number of critical locations outside the fuel tank. This AD requires installing additional and improved fuel system bonding provisions, and revising the airplane maintenance or inspection program, as applicable, by incorporating fuel airworthiness limitation items and critical design configuration control limitations. We are issuing this AD to prevent an ignition source in the fuel tank vapor space, which could result in a fuel tank explosion and consequent loss of the airplane.